Dynamic Stress Engineer

1.Conduct research and computational analysis on the flutter characteristics of primary aircraft structures.

2.Perform computational analysis of aircraft structural stiffness characteristics and simulation analysis of vibration characteristics.

3.Execute full-aircraft modal testing and vibration testing.

4.Analyze aeroelastic and servoelastic stability of the aircraft.

5.Prepare relevant technical documentation, including strength analysis reports and test reports.

1.Bachelor’s degree or above in Aerospace Engineering, Mechanical Engineering, Mechanics, or related fields. Proficiency in composite material structural strength analysis is preferred.

2.5+ years of experience in aircraft dynamic stress/dynamics analysis. Experience with general aviation aircraft or ton-class UAVs is preferred; experience with airworthiness certification is preferred.

3.Solid understanding of fundamental vibration theory, simulation analysis methods, and testing techniques.

4.Proficient in using dynamics-related simulation and testing software.

5.Strong English reading comprehension skills.

6.Strong ability to work under pressure, excellent communication and cross-departmental collaboration skills, high sense of responsibility, and a strong team player.